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EWS-G3

NORAD 35491 Payload GEO 2009-033A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35834 km
Apogee
35852 km
Inclination
1.9°
Period
1439.0 min
Mean Motion
1.00071290 rev/day
TLE Epoch
2026-09-17 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,843 km
Orbital Velocity11,062 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,214 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NOAA (National Oceanographic and Atmospheric Administration) (United States)
Launch Date
2009-06-27
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2009-033A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EWS-G3 is an active satellite operated by NOAA (National Oceanographic and Atmospheric Administration) (United States), launched on 2009-06-27 from Cape Canaveral Space Force Station, United States on the GOES O launch. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,834 km and 35,852 km with an inclination of 1.9°. It travels at approximately 11,062 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks EWS-G3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EWS-G3 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 1.9°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of EWS-G3’s average altitude, there are currently 108 active payloads and 43 tracked debris or rocket body fragments. United States operates approximately 13,204 active satellites in total, of which 18 share a similar altitude band with EWS-G3.
❓ Frequently Asked Questions
EWS-G3 orbits at approximately 35,843 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,062 km/h — it just keeps pace with the ground below. With an inclination of 1.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EWS-G3 is operated by NOAA (National Oceanographic and Atmospheric Administration) (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35491. You can track EWS-G3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EWS-G3 was launched on 2009-06-27 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks EWS-G3 (NORAD ID 35491) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
EWS-G3 travels at approximately 11,062 km/h (6,874 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.